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LYRA Instrument and Data Manager Software Requirements Analysis

LYRA Instrument and Data Manager Software Requirements Analysis. Concept description LIM requirements presentation (SBI) LDM requirements presentation (SBI) Interface issues Open questions. Agenda. Concept description. PROBA 2 orbit Sun synchronous LTAN: 6:00

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LYRA Instrument and Data Manager Software Requirements Analysis

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  1. LYRA Instrument and Data ManagerSoftware Requirements Analysis

  2. Concept description LIM requirements presentation (SBI) LDM requirements presentation (SBI) Interface issues Open questions Agenda

  3. Concept description • PROBA 2 orbit • Sun synchronous • LTAN: 6:00 • See emails F.Teston for details • Eclipses: • approximately 3 months eclipse season • rest of the year: no eclipses • maximum eclipse duration approx. 1100 sec.

  4. Ysun Xsun Rsc Sun Earth Rsun Concept description PROBA 2 Pointing 1. Frames definitions Sun frame (Xsun, Ysun, Zsun) Xsun is spacecraft-sun axis ( = unit(Rsun – Rsc) where Rsun is the apparent sun vector from the Earth (Sun ephemeris) and Rsc is the spacecraft position vector. If S/C position is unknown onboard, Rsc is set to zero. Ysun is perpendicular to Xsun, in the plane defined by Xsun and the normal to the ecliptic plane, pointing towards the northern hemisphere.

  5. Concept description S/C Fixed Body Frame Mechanical frame(Xmech, Ymech, Zmech)... With respect to S/C Payload frame(Xpl, Ypl, Zpl)...With respect to SWAP Spacecraft fixed body frame (Xbof, Ybof, Zbof) ... Related to Payload frame, but origin in S/C COG. Reference frame for spacecraft attitude control.

  6. Concept description • PROBA 2 Pointing • 2. Pointing in observation mode • ·four (baseline, up to 8 possible)large-angle rotations of 90° (or 360° / number of rotations) attitudes are commanded over one orbit in order to avoid blinding of the star trackers; For the rest of presentation: baseline number of rotations assumed) • ·the timing of the manoeuvres is such that the exclusion angles from the star trackers towards the earth are maximised; (performed on board -> cont. variation) • ·the 90° manoeuvres will take a few minutes and will be centred around these optimal switching times; • ·the time until the next rotation is continuously provided; • ·paving rotations are defined in the original sun frame.

  7. Concept description • PROBA 2 Pointing • 2. Pointing in observation mode • The observation mode is commanded as follows: • the large rotation is commanded as a quaternion in the SUN frame: [q1cmd, 0, 0, q4cmd]; • the commanded large angle rotations will be taken from a list (of maximum 8) quaternions, configured by the ground; • the index of the currently used large angle rotation will continuously be provided; • the paving rotation is commanded as a quaternion in the SUN frame: [0, q2paving, q3 paving, q4 paving]

  8. Concept description • LIM mode diagram

  9. Mode simplification: Off (CSL/ROB survival mode -> idem SWAP) Idle (CSL/ROB night mode -> idem SWAP) Warm-up (CSL/ROB stand-by mode -> idem SWAP) Acquisition (CSL/ROB nominal modes) Modes not implemented in SWIM: First swtich on: will be performed by uploaded procedure Bake-out mode: uploaded or onboard procedure Calibration mode: uploaded or onboard procedure, using manually the imaging mode with different pointing configurations Concept description

  10. Concept description • Sequence diagram Nominal observation

  11. Concept description

  12. Concept description

  13. Concept description

  14. Open questions

  15. Interace issues

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